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Title:
民間航空機用方向舵
Document Type and Number:
Japanese Patent JP4820878
Kind Code:
B2
Abstract:
A rudder of a commercial aircraft is provided that is divided along its longitudinal direction in at least one region and the parts of the rudder can be spread against the air flow surrounding the aircraft by means of an actuator in order to decelerate the aircraft.

Inventors:
Bender Klaus
Application Number:
JP2008544858A
Publication Date:
November 24, 2011
Filing Date:
December 12, 2006
Export Citation:
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Assignee:
Airbus Opera Zion Gesellschaft Mitt Beschlenktel Haftung
International Classes:
B64C9/32; B64C5/06; B64C23/06
Domestic Patent References:
JPH0232000A1990-02-01
Foreign References:
US2643833A1953-06-30
US4290612A1981-09-22
GB722842A1955-02-02
EP1527992A22005-05-04
US3120935A1964-02-11
US2241335A1941-05-06
Attorney, Agent or Firm:
Masayuki Masabayashi
Hayashi Ichiyoshi



 
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